System and method for detecting operating events of an engine via midi

ABSTRACT

A method of monitoring an operating event of a combustion engine includes receiving a noise signal sensed by a knock sensor disposed in or proximate to the combustion engine, correlating the noise signal with a musical instrument digital interface (MIDI) fingerprint having at least an ADSR envelope indicative of the operating event, and detecting if the operating event has occurred based on the correlating of the noise signal with the fingerprint.

The subject matter disclosed herein relates to fuel combusting enginesand, more specifically, to a system and method for detecting operatingevents and conditions of a reciprocating engine using a knock sensor,for example, via musical instrument digital interface (MIDI).

Combustion engines typically combust a carbonaceous fuel, such asnatural gas, gasoline, diesel, and the like, and use the correspondingexpansion of high temperature and pressure gases to apply a force tocertain components of the engine, e.g., piston disposed in a cylinder,to move the components over a distance. Each cylinder may include one ormore valves that open and close correlative with combustion of thecarbonaceous fuel. For example, an intake valve may direct an oxidizersuch as air into the cylinder, which is then mixed with fuel andcombusted. Combustion fluids, e.g., hot gases, may then be directed toexit the cylinder via an exhaust valve. Accordingly, the carbonaceousfuel is transformed into mechanical motion, useful in driving a load(e.g., a generator that produces electric power). In traditionalconfigurations, timing of opening and closing the intake and exhaustvalves during operation of the combustion engine may be monitored andestimated using traditional techniques. Traditional techniques may alsobe used for detecting certain other operating events and conditions(e.g., peak firing pressure) of the combustion engine. However,traditional monitoring techniques may not be accurate, and correctivemeasures utilizing the traditional monitoring techniques may reduce anefficiency of the internal combustion engine. Accordingly, improvedmonitoring of operating events and conditions, such as peak firingpressure and/or intake and exhaust valve closure (or opening) operatingevents, may be useful.

BRIEF DESCRIPTION

Certain embodiments commensurate in scope with the originally claimedinvention are summarized below. These embodiments are not intended tolimit the scope of the claimed invention, but rather these embodimentsare intended only to provide a brief summary of possible forms of thepresent disclosure. Indeed, the present disclosure may encompass avariety of forms that may be similar to or different from theembodiments set forth below.

In a first embodiment, a method of monitoring an operating event of acombustion engine includes receiving a noise signal sensed by a knocksensor disposed in or proximate to the combustion engine, correlatingthe noise signal with a musical instrument digital interface (MIDI)fingerprint having at least an ADSR envelope indicative of the operatingevent, and detecting if the operating event has occurred based on thecorrelating of the noise signal with the fingerprint.

In a second embodiment, a system includes an engine controllerconfigured to monitor a first operating event of a combustion engine.The controller includes a processor configured receive a noise signalsensed by a knock sensor disposed in or proximate to the combustionengine, correlate the noise signal with a first musical instrumentdigital interface (MIDI) fingerprint having at least a first ADSRenvelope indicative of the first operating event, and detect if theoperating event has occurred based on the correlating of the noisesignal with the first fingerprint.

In a third embodiment, a non-transitory computer readable mediumincludes executable instructions that, when executed, cause a processorto receive, from a knock sensor disposed in or proximate to an internalcombustion engine, noise data indicative of noise emitted by theinternal combustion engine. The executable instructions, when executed,also cause the processor to receive, from a crankshaft sensor disposedin or proximate to the combustion engine, crank angle data indicative ofa crank angle of a crankshaft of the internal combustion engine.Further, the executable instructions, when executed, cause the processorto plot the noise data against the crank angle data, determine a portionof the noise data that corresponds to a musical instrument digitalinterface (MIDI) fingerprint having a reference ADSR envelope indicativeof an operating event of the internal combustion engine, superimpose thereference ADSR envelope over the portion of the noise data, anddetermine a location in the noise data at which the operating eventoccurred.

BRIEF DESCRIPTION OF THE DRAWINGS

These and other features, aspects, and advantages of the presentinvention will become better understood when the following detaileddescription is read with reference to the accompanying drawings in whichlike characters represent like parts throughout the drawings, wherein:

FIG. 1 is a block diagram of an embodiment of a portion of an enginedriven power generation system in accordance with aspects of the presentdisclosure;

FIG. 2 is a side cross-sectional view of an embodiment of a pistonassembly within a cylinder of the reciprocating engine shown in FIG. 1in accordance with aspects of the present disclosure;

FIG. 3 is an embodiment of an engine noise plot of data measured by theknock sensor shown in FIG. 2 in accordance with aspects of the presentdisclosure;

FIG. 4 is an embodiment of a scaled version of the sample engine noiseplot shown in FIG. 3 in accordance with aspects of the presentdisclosure;

FIG. 5 is an embodiment of a sample scaled engine noise plot shown inFIG. 4 with four principle parameters of an attack, decay, sustain,release (ADSR) envelope overlaid in accordance with aspects of thepresent disclosure;

FIG. 6 is an embodiment of a scaled engine noise plot and ADSR envelopeshown in FIG. 5 with the extracted tones overlaid in accordance withaspects of the present disclosure;

FIG. 7 is a flow chart showing an embodiment of a process forcharacterizing a noise in accordance with aspects of the presentdisclosure;

FIG. 8 is a an embodiment of a scaled engine noise plot corresponding toan engine operating event, an operating event indicator corresponding tothe engine operating event, and an ADSR envelope corresponding to theengine operating event in accordance with the process of FIG. 7 andother aspects of the present disclosure;

FIG. 9 is a flow chart showing an embodiment of a process foridentifying a fingerprint shown in FIG. 7 in accordance with aspects ofthe present disclosure;

FIG. 10 is a flow chart of an embodiment of a process suitable forprocessing engine noise to derive certain engine operating events; and

FIG. 11 is a flow chart of an embodiment of a process suitable forderiving and using MIDI data.

DETAILED DESCRIPTION

One or more specific embodiments of the present invention will bedescribed below. In an effort to provide a concise description of theseembodiments, all features of an actual implementation may not bedescribed in the specification. It should be appreciated that in thedevelopment of any such actual implementation, as in any engineering ordesign project, numerous implementation-specific decisions must be madeto achieve the developers' specific goals, such as compliance withsystem-related and business-related constraints, which may vary from oneimplementation to another. Moreover, it should be appreciated that sucha development effort might be complex and time consuming, but wouldnevertheless be a routine undertaking of design, fabrication, andmanufacture for those of ordinary skill having the benefit of thisdisclosure.

When introducing elements of various embodiments of the presentinvention, the articles “a,” “an,” “the,” and “said” are intended tomean that there are one or more of the elements. The terms “comprising,”“including,” and “having” are intended to be inclusive and mean thatthere may be additional elements other than the listed elements.

The disclosed embodiments employ sensors (e.g., knock sensors, acousticsensors, or vibration sensors) and baseline data (e.g., fingerprints ofsound or vibration) to monitor, diagnose, and/or control an engine. Incertain embodiments, a musical instrument digital interface (MIDI)format is used to store, transmit, and/or analyze the data describedherein, including knock sensor data, baselines, fingerprints, and thelike. When using a knock sensor to monitor a combustion engine,occasionally the knock sensor system records a noise, such as anabnormal or undesired noise that may not be identified at that time.Alternatively, the knock sensor may record a noise that is a normal ordesired noise, where the noise has been previously identified andcharacterized. For example, noises emitted by the combustion engineduring various actions by the combustion engine may be initiallycharacterized during an in-factory baselining process. Noise signals forparticular operating events and conditions (e.g., valve closures, valveopenings, and peak firing pressure) during the baselining process may beprocessed and stored in a database as relating to one or more operatingevents. During normal operation of the combustion engine, data stored inthe database relating to the operating events characterized during thebaselining process may be accessed to determine if operational noisecorresponds to the operating events characterized during the baseliningprocess.

Advantageously, the techniques described herein may create a sound“fingerprint” of certain engine sounds or noise, via MIDI techniques.The fingerprint (e.g., profile, comparator, and/or reference signal) maybe developed during the baselining process, as described above, and thefingerprint may correspond to a particular operating event (e.g., avalve closure) tested during the baselining process. It should be notedthat the baselining process may be carried out during full operation ofthe combustion engine or while only operating certain components (e.g.,the components relating to the operating event(s) being baselined) ofthe combustion engine. For example, in some embodiments, variousoperating events of the combustion engine may be baselined in-factoryduring part or full operation.

During full operation of the combustion engine (e.g., after baselining),noise may be detected by the knock sensor, and the noise signal may beprocessed, e.g., via MIDI techniques, and compared to variousfingerprints (e.g., profiles, signatures, comparators, referencesignals, unique indicia, unique representations, etc. stored in a MIDIfile format) relating to the combustion engine. If the fingerprint andthe processed noise signal correspond or correlate (e.g., “match”), thesignal may be confirmed as corresponding to the operating event relatingto the fingerprint. The noise signal may also be processed to determinetime-sensitive information relating to the operating event thatcorresponds to the matched fingerprint and noise signal. For example, ifthe noise signal matches a fingerprint corresponding to closure of anexhaust valve, the noise signal may be plotted with respect to time (orcrank angle) to determine when the exhaust valve closed.

As described in further detail below, systems and method are providedfor identifying and classifying noise via anAttack-Decay-Sustain-Release (ADSR) envelope and/or joint time-frequencytechniques, where the ADSR envelope may correspond to at least a portionof the above-referenced fingerprint. The joint time-frequency techniquesmay include cepstrum techniques, frequency techniques, chirplettechniques, and/or wavelet techniques to develop an acoustic model orfingerprint of the noise, as described in more detail below.

Turning to the drawings, FIG. 1 illustrates a block diagram of anembodiment of a portion of an engine driven power generation system 8.As described in detail below, the system 8 includes an engine 10 (e.g.,a reciprocating internal combustion engine) having one or morecombustion chambers 12 (e.g., 1, 2, 3, 4, 5, 6, 7, 8, 10, 12, 14, 16,18, 20, or more combustion chambers 12). An air supply 14 is configuredto provide a pressurized oxidant 16, such as air, oxygen,oxygen-enriched air, oxygen-reduced air, or any combination thereof, toeach combustion chamber 12. The combustion chamber 12 is also configuredto receive a fuel 18 (e.g., a liquid and/or gaseous fuel) from a fuelsupply 19, and a fuel-air mixture ignites and combusts within eachcombustion chamber 12. The hot pressurized combustion gases cause apiston 20 adjacent to each combustion chamber 12 to move linearly withina cylinder 26 and convert pressure exerted by the gases into a rotatingmotion, which causes a shaft 22 to rotate. Further, the shaft 22 may becoupled to a load 24, which is powered via rotation of the shaft 22. Forexample, the load 24 may be any suitable device that may generate powervia the rotational output of the system 10, such as an electricalgenerator. Additionally, although the following discussion refers to airas the oxidant 16, any suitable oxidant may be used with the disclosedembodiments. Similarly, the fuel 18 may be any suitable gaseous fuel,such as natural gas, associated petroleum gas, propane, biogas, sewagegas, landfill gas, coal mine gas, for example.

The system 8 disclosed herein may be adapted for use in stationaryapplications (e.g., in industrial power generating engines) or in mobileapplications (e.g., in cars or aircraft). The engine 10 may be atwo-stroke engine, three-stroke engine, four-stroke engine, five-strokeengine, or six-stroke engine. The engine 10 may also include any numberof combustion chambers 12, pistons 20, and associated cylinders (e.g.,1-24). For example, in certain embodiments, the system 8 may include alarge-scale industrial reciprocating engine having 4, 6, 8, 10, 16, 24or more pistons 20 reciprocating in cylinders. In some such cases, thecylinders and/or the pistons 20 may have a diameter of betweenapproximately 13.5-34 centimeters (cm). In some embodiments, thecylinders and/or the pistons 20 may have a diameter of betweenapproximately 10-40 cm, 15-25 cm, or about 15 cm. The system 10 maygenerate power ranging from 10 kW to 10 MW. In some embodiments, theengine 10 may operate at less than approximately 1800 revolutions perminute (RPM). In some embodiments, the engine 10 may operate at lessthan approximately 2000 RPM, 1900 RPM, 1700 RPM, 1600 RPM, 1500 RPM,1400 RPM, 1300 RPM, 1200 RPM, 1000 RPM, 900 RPM, or 750 RPM. In someembodiments, the engine 10 may operate between approximately 750-2000RPM, 900-1800 RPM, or 1000-1600 RPM. In some embodiments, the engine 10may operate at approximately 1800 RPM, 1500 RPM, 1200 RPM, 1000 RPM, or900 RPM. Exemplary engines 10 may include General Electric Company'sJenbacher Engines (e.g., Jenbacher Type 2, Type 3, Type 4, Type 6 orJ920 FleXtra) or Waukesha Engines (e.g., Waukesha VGF, VHP, APG, 275GL),for example.

The driven power generation system 8 may include one or more knocksensors 23 suitable for detecting engine “knock.” The knock sensor 23may be any sensor configured to sense sounds or vibrations caused by theengine 10, such as sound or vibration due to detonation, pre-ignition,and or pinging. The knock sensor 23 is shown communicatively coupled toan engine control unit (ECU) 25. During operations, signals from theknock sensor 23 are communicated to the ECU 25 to determine if knockingconditions (e.g., pinging) exist. The ECU 25 may then adjust certainengine 10 parameters to ameliorate or eliminate the knocking conditions.For example, the ECU 25 may adjust ignition timing and/or adjust boostpressure to eliminate the knocking. As further described herein, theknock sensor 23 may additionally derive that certain sounds orvibrations should be further analyzed and categorized to detect, forexample, undesired engine conditions.

FIG. 2 is a side cross-sectional view of an embodiment of a pistonassembly 25 having a piston 20 disposed within a cylinder 26 (e.g., anengine cylinder) of the reciprocating engine 10. The cylinder 26 has aninner annular wall 28 defining a cylindrical cavity 30 (e.g., bore). Thepiston 20 may be defined by an axial axis or direction 34, a radial axisor direction 36, and a circumferential axis or direction 38. The piston20 includes a top portion 40 (e.g., a top land). The top portion 40generally blocks the fuel 18 and the air 16, or a fuel-air mixture 32,from escaping from the combustion chamber 12 during reciprocating motionof the piston 20.

As shown, the piston 20 is attached to a crankshaft 54 via a connectingrod 56 and a pin 58. The crankshaft 54 translates the reciprocatinglinear motion of the piston 24 into a rotating motion. As the piston 20moves, the crankshaft 54 rotates to power the load 24 (shown in FIG. 1),as discussed above. As shown, the combustion chamber 12 is positionedadjacent to the top land 40 of the piston 24. A fuel injector 60provides the fuel 18 to the combustion chamber 12, and an intake valve62 controls the delivery of air 16 to the combustion chamber 12. Anexhaust valve 64 controls discharge of exhaust from the engine 10.However, it should be understood that any suitable elements and/ortechniques for providing fuel 18 and air 16 to the combustion chamber 12and/or for discharging exhaust may be utilized, and in some embodiments,no fuel injection is used. In operation, combustion of the fuel 18 withthe air 16 in the combustion chamber 12 cause the piston 20 to move in areciprocating manner (e.g., back and forth) in the axial direction 34within the cavity 30 of the cylinder 26.

During operations, when the piston 20 is at the highest point in thecylinder 26 it is in a position called top dead center (TDC). When thepiston 20 is at its lowest point in the cylinder 26, it is in a positioncalled bottom dead center (BDC). As the piston 20 moves from top tobottom or from bottom to top, the crankshaft 54 rotates one half of arevolution. Each movement of the piston 20 from top to bottom or frombottom to top is called a stroke, and engine 10 embodiments may includetwo-stroke engines, three-stroke engines, four-stroke engines,five-stroke engine, six-stroke engines, or more.

During engine 10 operations, a sequence including an intake process, acompression process, a power process, and an exhaust process occurs. Theintake process enables a combustible mixture, such as fuel and air, tobe pulled into the cylinder 26, thus the intake valve 62 is open and theexhaust valve 64 is closed. The compression process compresses thecombustible mixture into a smaller space, so both the intake valve 62and the exhaust valve 64 are closed. The power process ignites thecompressed fuel-air mixture, which may include a spark ignition througha spark plug system, and/or a compression ignition through compressionheat. The resulting pressure from combustion then forces the piston 20to BDC. The exhaust process typically returns the piston 20 to TDC whilekeeping the exhaust valve 64 open. The exhaust process thus expels thespent fuel-air mixture through the exhaust valve 64. It is to be notedthat more than one intake valve 62 and exhaust valve 64 may be used percylinder 26.

The depicted engine 10 also includes a crankshaft sensor 66, the knocksensor 23, and the engine control unit (ECU) 25, which includes aprocessor 72 and memory 74. The crankshaft sensor 66 senses the positionand/or rotational speed of the crankshaft 54. Accordingly, a crank angleor crank timing information may be derived. That is, when monitoringcombustion engines, timing is frequently expressed in terms ofcrankshaft 54 angle. For example, a full cycle of a four stroke engine10 may be measured as a 720° cycle. The knock sensor 23 may be aPiezo-electric accelerometer, a microelectromechanical system (MEMS)sensor, a Hall effect sensor, a magnetostrictive sensor, and/or anyother sensor designed to sense vibration, acceleration, sound, and/ormovement. In other embodiments, sensor 23 may not be a knock sensor inthe traditional sense, but any sensor that may sense vibration,pressure, acceleration, deflection, or movement, and may not be used todetect engine “knock.”

Because of the percussive nature of the engine 10, the knock sensor 23may be capable of detecting signatures even when mounted on the exteriorof the cylinder 26. However, the knock sensor 23 may be disposed atvarious locations in or about the cylinder 26. Additionally, in someembodiments, a single knock sensor 23 may be shared, for example, withone or more adjacent cylinders 26. In other embodiments, each cylinder26 may include one or more knock sensors 23. The crankshaft sensor 66and the knock sensor 23 are shown in electronic communication with theengine control unit (ECU) 25. The ECU 25 includes a processor 72 and amemory 74. The memory 74 may store computer instructions that may beexecuted by the processor 72. The ECU 25 monitors and controls andoperation of the engine 10, for example, by adjusting combustion timing,valve 62, 64, timing, adjusting the delivery of fuel and oxidant (e.g.,air), and so on.

Advantageously, the techniques described herein may use the ECU 25 toreceive data from the crankshaft sensor 66 and the knock sensor 23, andthen to create a “noise” signature, such as a MIDI-based signature, byplotting the knock sensor 23 data against the crankshaft 54 position.The ECU 25 may then go through the process of analyzing the data toderive normal (e.g., known and expected noises) and abnormal signatures(e.g., unknown or unexpected noises). The ECU 25 may then characterizethe signatures, as described in more detail below. By providing forsignature analysis, such as MIDI-based signature analysis, thetechniques described herein may enable a more optimal and a moreefficient operation and maintenance of the engine 10.

MIDI techniques enable a more compact storage and/or transmission forcertain of the data described herein, such as fingerprint data, datareceived via the knock sensor(s) 23, and the like. For example,fingerprint data, knock sensor data, and the like, may be converted intoMIDI data for storage, transmission, and/or processing. The MIDI datamay specify a notation, a pitch and velocity for certain music notes.MIDI data may also include control signals for parameters such asvolume, vibrato, audio panning, cues, and clock signals that may set andsynchronize tempo. The MIDI data may include one or more channels ofdata, such as between 1 to 32 channels of data. Applying MIDI techniquescarries certain advantages, which include file compactness (sound datacan be coded in a few hundred lines or thousand lines, e.g., inkilobytes, as opposed to megabytes or gigabytes), ease of modificationand manipulation. Indeed, unlike digital or analog recordings of soundor vibration, MIDI symbolically represents a note and not a recording ofthe note (or of sound) itself. Because the actual sound is not recordedby rather represented symbolically, MIDI may be a lossy encoding asopposed to lossless encoding. MIDI files describe herein may be instandard MIDI file formats type 0, type 1, and/or type 2. It is to benoted that while the embodiments described herein refer to MIDItechniques, other techniques for symbolically representing sounds orvibrations as opposed to actual recordings of the sounds or vibrationsmay be used, including MusicXML, MuseData, notation interchange fileformat (NIFF), XEMO, Csound, Final, SharpEye, FreeHand, and so on.

FIGS. 3-6 and 8 are illustrative of data that may be undergoing dataprocessing, for example, via a process or processes described in moredetail with respect to FIGS. 7 and 9. The data for FIGS. 3-6 and 8 mayinclude data transmitted via the knock sensor 23 and the crankshaftsensor 66. For example, FIG. 3 is an embodiment of a raw engine noiseplot 75 derived (e.g., by the ECU 25) of noise data measured by theknock sensor 23 in which x-axis 76 is crankshaft 54 position (e.g.,crank angle), which is correlative of time. In accordance with presentembodiments, the noise data may correspond to a particular operatingevent or action of the engine 10. For example, the noise data maycorrespond to opening or closing of a valve of the engine 10, forexample, the exhaust valve 64. Alternatively, the noise data maycorrespond to peak firing pressure, which describes the highest pressurein the combustion chamber 12 during combustion.

The plot 75 is generated when the ECU 25 combines the data received fromthe knock sensor 23 and the crankshaft sensor 66 during operations ofthe engine 10. In the depicted embodiment, an amplitude curve 77 of theknock sensor 23 signal is shown, with an amplitude axis 78. That is, theamplitude curve 77 includes amplitude measurements of vibration data(e.g., noise, sound data) sensed via the knock sensor 23 plotted againstcrank angle. It should be understood that this is merely a plot of asample data set (e.g., corresponding to closure of the exhaust valve64), and not intended to limit plots generated by the ECU 25. The curve77 may be encoded as MIDI data 91 and then stored in a MIDI file. Forexample, as the knock sensor(s) 23 transmit a signal, the signal may beprocessed (e.g., via the ECU 25) to derive corresponding MIDI “sounds”(e.g., notation, a pitch and velocity for certain music notes, and/orcontrol signals for parameters such as volume, vibrato, audio panning,cues, and clock signals that may set and synchronize tempo) and encodedinto the MIDI data 91. The curve 77, which may now be encoded as MIDIdata 91, may then be scaled for further processing, as shown in FIG. 4.

FIG. 4 is an embodiment of a scaled engine noise plot 79, which may bederived by the ECU 25. In the scaled plot 79, the raw engine noise fromamplitude plot 75 shown in FIG. 3 has been scaled to derive a scaledamplitude curve 80. In certain embodiments, the MIDI data 91 encoded inone or more MIDI files may be scaled, such as via a multiplier ormultipliers to the various sounds or notes. In other embodiments, thecurve 77 may not be converted to MIDI but may instead be scaled firstand then the scaled curve may be converted to MIDI.

In either case, a single multiplier has been applied to each data point(when not converted to MIDI data) or note (when converted to MIDI data)such that the maximum positive value of the scaled amplitude curve 80is 1. Note that the multiplier applied to each point or note of curve 80in order to produce a maximum positive value of 1 may result in negativevalues that are less than or greater than −1. That is, for example, themaximum negative value may be −0.5, or it may be −1.9, as shown inscaled engine noise plot 79 shown in FIG. 4. The figure also shows thecurve 80 encoded as a MIDI data 93. As mentioned earlier, vibration orsound curves, such as the curve 80, may be processed (e.g., via the ECU25) to derive corresponding MIDI “sounds” (e.g., notation, a pitch andvelocity for certain music notes, and/or control signals for parameterssuch as volume, vibrato, audio panning, cues, and clock signals that mayset and synchronize tempo) and encoded into MIDI files, such as via MIDIdata 93.

FIG. 5 is an embodiment of a scaled engine noise plot 81 with fourprinciple parameters of an attack, decay, sustain, release (ADSR)envelope 82 laid over the top of the plot. The ADSR envelope 82 istypically used in music synthesizers in order to mimic the sound ofmusical instruments. Advantageously, the techniques described hereinapply the ADSR envelope 82 to knock sensor 23 data to more quickly andefficiently provide for certain noise analysis, as further describedbelow. For example, the scaled curve 80 may be characteristic (orinclude characteristics) of a particular operating event (e.g., valve62, 64 opening/closing or peak firing pressure in the combustion chamber12) of the engine 10, and the ADSR envelope 82 developed for the scaledcurve 80 may be utilized for future analysis of the operating eventduring operation of the engine 10. As for all plots or curves in allfigures herein, plot 81 may be processed, stored, and/or transmitted asMIDI data, for example as MIDI data 95.

The four principle parameters of the ADSR envelope are attack 83, decay84, sustain 85, and release 86. The attack 83 occurs from the start ofthe noise to a peak amplitude 87 of the scaled curve 80. The decay 84occurs in the run down from the peak amplitude to a designated sustain85 level, which may be some specified percent of the maximum amplitude.It should be understood that the order of the four parameters does nothave to be attack, decay, sustain, and release. For example, for somenoises, the order may be attack, sustain, decay, and release. In suchcases, an ADSR, rather than ADSR, envelope would be applied. For thesake of simplicity, this will be referred to as an “ADSR envelope,” butit should be understood that the term applies to a noise regardless ofthe order of the parameters. The sustain 85 level is the main levelduring the noise's duration. In some embodiments, the sustain 85 levelmay occur at 55% of the maximum amplitude. In other embodiments, thesustain 85 level may be at least equal to or greater than 35%, 40%, 45%,50%, 60%, or 65% of the maximum amplitude. A user, or the ECU 25, maycheck whether the sustain level is as desired by determining whether thesustain 85 level is held for at least 15% of the duration of thesignature. If the sustain 85 lasts more than 15% of the duration of thesignature, the sustain 85 level is set as desired. The release 86 occursduring the run down from the sustain 85 level back to zero. It should benoted that, in some embodiments, the noise signal (e.g., the scaledamplitude curve 80) may be filtered via a high-pass filter, a low-passfilter, or a band-pass filter to attenuate portions of the signal havingfrequencies uncharacteristic of the operating event. The particularfilter applied to the noise signal may depend on the operating eventbeing monitored. For example, when monitoring valve 62, 64 events (e.g.,openings and closures), a high-pass filter (e.g., greater than 10kilohertz (kHz)) or a band-pass filter (e.g., between 10 and 20kilohertz (kHz)) may be applied to the noise signal. When monitoringcombustion events (e.g., peak firing pressure), a low-pass filter (e.g.,less than 2 kilohertz (kHz)) may be applied to the noise signal.

FIG. 6 shows the same scaled engine noise plot 79 shown in FIGS. 4 and 5with certain tones overlaid (e.g., superimposed). After applying theADSR envelope 82, the ECU 25 may extract three to five of the strongestfrequencies in the noise and convert them into musical tones. Forexample, a lookup table mapping frequency ranges to musical tones may beused. Additionally or alternatively, equations may be used based on theobservation that pitch is typically perceived as the logarithm offrequency for equal temperament systems of tuning, or equations forother musical temperament systems. In other embodiments, more or lessfrequencies may be extracted. In the plot 81 shown in FIG. 6 the threeprominent (e.g., extracted) tones are C#5, E4, and B3. It should beunderstood, however, that these three tones are merely examples ofpossible tones and not intended to limit what tones may be present in arecorded noise. It is also to be noted that the extracted notes and orthe sounds for plot 81 may be encoded as MIDI data 97 and stored in MIDIfile(s).

FIG. 7 is a flow chart showing an embodiment of a process 88 forcharacterizing a noise, such as a noise sensed via the knock sensor 23.By characterizing the noise, the noise can be logged and sorted foranalysis, including future analysis and/or real-time analysis. Forexample, in some embodiments, the process 88 may be used forcharacterizing a noise relating to a particular operating event oraction of the engine 10, such as peak firing pressure or opening/closingof intake or exhaust valves 62, 64. Further, the noise may first becharacterized during a baselining process (e.g., an in-factorybaselining process including the use of MIDI encoding) before the engine10 is implemented for normal or full time operation, e.g., before beingsold, deployed to a site, implemented at a site, etc. For example,before normal operation of the engine 10, various operating events(e.g., peak firing pressure, intake/exhaust opening/closing) may betested by analyzing the noise emitted during the operating event(s) (anddetected by the knock sensor 23), where the noise signals or ADSRenvelopes 82 of the noise signals may be fingerprinted as relating tothe operating events being tested, thus creating a baseline. It shouldbe noted that the process 88 (e.g., baselining process) may be utilizedwhen the engine 10 is not fully operating to simplify processing of thenoise signal. For example, the process 88 may be utilized while onlyopening or closing a valve (e.g., the exhaust valve 64 or the intakevalve 82) to characterize the noise corresponding to the opening orclosing of the valve (e.g., the exhaust valve 64 or the intake valve82). In other embodiments, the process 88 may be utilized during partialor during full engine 10 operations.

In the illustrated embodiment, the process 88 may be implemented ascomputer instructions or executable code stored in the memory 74 andexecutable by the processor 72 of the ECU 25. In block 90, a sample ofdata is taken using the knock sensor 23 and the crankshaft sensor 66.For example, the sensors 66, 23 collect data of an operating event(e.g., closure of the exhaust valve 74) during baselining and thentransmit the data to the ECU 25. As previously described, the process 88may be a baselining process and may be carried out while only particularcomponents of the engine 10 are operating. For example, the process 88may be carried out while opening and/or closing the exhaust valve 64 (orintake valve 62), such that the noise emitted during, for example,closing of the exhaust valve 64 may be readily processed. The ECU 25then logs the crankshaft 54 angles at the start of data collection andat the end of data collection, as well as the time and/or crankshaftangle at the maximum (e.g., amplitude 87) and minimum amplitudes.Indeed, the crankshaft 54 angle may be logged continuously during thebaselining process, enabling continuous plotting of the noise dataagainst crankshaft 54 angle.

In block 92, the ECU 25 preconditions the knock sensor 23 data. Thisblock 92 includes plotting the raw knock sensor 23 data againstcrankshaft 54 position or angle (or, in some embodiments, against time).A sample raw engine noise plot was shown in FIG. 3 as the amplitude plot75, which may also be provided as MIDI data 91. This block 92 alsoincludes scaling the raw engine noise data. To scale the data, the ECU25 determines a multiplier that would result in a maximum amplitude ofpositive 1. It should be noted that the maximum negative value has noeffect on multiplier selection. The ECU 25 then multiplies each datapoint (e.g., data point or music note in amplitude curve 77) by themultiplier, to derive the scaled amplitude curve 80, as shown in FIG. 4,which may also include MIDI data 93. It should be understood that thescaled engine noise plot 79 in FIG. 4 showing the scaled amplitude curve80 is merely an example and not intended to limit the scope of thisdisclosure to plots that look the same or similar to scaled engine noiseplot 79.

In block 94, the ECU 25 applies the ADSR envelope 82 to the engine noisesignal. The processing in this block was discussed in describing FIG. 5,which may also include MIDI data 95 processing. The ADSR envelope 82 isused to divide a noise data set into four different parameters or phases(attack 83, decay 84, sustain 85, release 86). As previously discussed,it should be understood that the order of the four parameters does nothave to be attack, decay, sustain, and release. For example, for somenoises, the order may be attack, sustain, decay, and release, or anyother possible order. For the sake of simplicity, this will be referredto as an “ADSR envelope,” but it should be understood that the termapplies to a noise regardless of the order of the parameters.Traditionally, the ADSR envelope 82 is used in the process ofreproducing a musical sound like that of a trumpet. However, in thetechniques described herein, the ADSR envelope may be used to categorizeand characterize noises so they can be cataloged and sorted, either forlater analysis, real-time analysis, or some other purpose. The fourprinciple parameters of the ADSR envelope 82 are attack 83, decay 84,sustain 85, and release 86. The attack 83 occurs from the start of thenoise to the peak amplitude 87. The decay 84 occurs in the run down fromthe peak amplitude 87 to a designated sustain 85 level, which is somespecified percent of the maximum amplitude. The sustain 85 level is themain level during the noise's duration. In some embodiments, the sustain85 level may occur at 55% of the maximum amplitude. In otherembodiments, the sustain 85 level may be at least equal to or greaterthan 35%, 40%, 45%, 50%, 60%, or 65% of the maximum amplitude. A user,or the ECU 25, may check whether the sustain level is as desired bydetermining whether the sustain 85 level is held for at least 15% of theduration of the signature. If the sustain 85 lasts more than 15% of theduration of the signature, the sustain 85 level is set as desired. Therelease 86 occurs during the run down from the sustain 85 level back tozero. In block 94 the ECU 25 measures the time from zero to maximumamplitude 87 (the maximum amplitude should have a value of 1). The ECU25 then measures the run down time from the maximum amplitude 87 to thedesignated sustain level 85. The ECU 25 then measures the level and timethat the noise sustains. Finally, the ECU 25 measures the time it takesfor the noise to run down from the sustain level 85 to zero. The ECU 25then logs the ADSR vectors or segments defining the ADSR envelope 82.

In block 96, the ECU 25 derives tonal information (e.g., musical tones)from the data. This block was discussed in the description of FIG. 6.During this block, the ECU 25, extracts tonal information from the data,identifying, for example, the three to five strongest tones in the data.In another embodiment, any number of tones may be identified, e.g., 1,2, 3, 4, 5, 6, 7, 8, 9, 10, or more tones. FIG. 6 shows three tonesderived from the signal, C#5, E4, and B3. The ECU 25 may derive five ormore tones from the data. Though FIG. 6 shows tones C#5, E4, and B3, itshould be understood that these tones are examples and the ECU 25 mayderive any tones from the data, including MIDI data 97. The ECU 25 thenlogs the derived tonal information, which may include the frequency ofthe fundamental derived tones (i.e., the lowest frequency tones), theorder of the fundamental derived tones, the frequency of the harmonicderived tones (i.e., tones with a frequency that is an integer multipleof the fundamental frequency), the order of the harmonic derived tones,and any other relevant tonal information.

In block 98, the ECU 25 creates a fingerprint, such as a MIDIfingerprint 100 based upon the ADSR envelope 82 and the tonalinformation derived in blocks 94 and 96. The MIDI fingerprint 100includes a symbolic MIDI-based characterization of the noise, breakingthe noise up into its component parts (e.g., ADSR envelope 82 components83, 84, 85, 86, which may help identify valve opening/closing eventsand/or peak firing pressure) and quantifying those parts so the noisecan be cataloged, categorized, and sorted. At this point in the process,the MIDI fingerprint 100 is based mostly upon the ADSR envelope in block94 and the tonal information derived in block 96.

In block 102, the MIDI fingerprint 100 is identified and checked. Usinga number of techniques, which will be described later, the MIDIfingerprint 100 may be modified or added to and then checked again. Itshould be noted that, as previously described, the MIDI fingerprint 100may be logged with reference to a particular operating event or actionof the engine 10. For example, the process 88 may correspond to abaselining process that characterizes noise signals relative toparticular operating events that may occur during operation of theengine 10. In particular, the noise signal detected during the process88 may relate to peak firing pressure, closure or opening of the exhaustvalve 64, closure or opening of the intake valve 62, or a combinationthereof. The fingerprint 100 may be stored in the memory 74 of the ECU25 as corresponding to the particular operating event or condition beingtested (e.g., baselined).

In some embodiments, the process 88 (e.g., baselining process) mayinclude one or more additional steps that further processes the noisesignal or ADSR envelope 82 to provide additional information relating tothe operating event (e.g., opening or closing of the exhaust or intakevalves 64, 62) or action of the engine 10. For example, for clarity,FIG. 8 is an embodiment of a scaled engine noise plot 81 with a scaledamplitude curve 80 corresponding to an engine operating event (e.g.valve opening or closing event), an operating event indicator 103corresponding to the engine operating event, and an ADSR envelope 82corresponding to the engine operating event in accordance with theprocess of FIG. 7. It should be noted, that the curve 80 may be stored,transmitted, and/or processed as MIDI data 99, and that as previouslydescribed, the engine operating event and the corresponding plot 81 inFIG. 8 may be tested (e.g., baselined via the process 88) while theengine 10 is not fully operating. Thus, the fluctuations in theillustrated amplitude curve 80 occur at predictable times correspondingto the operating event, and enable simpler processing. In other words,in some embodiments, no components or operating events of the engine 10may emit noise other than the components or operating events beingtested (e.g., baselined). Additionally or alternatively, the noisesignal may be filtered via a high-pass filter, a low-pass filter, or aband-pass filter to attenuate portions of the signal having frequenciesuncharacteristic of the operating event. The particular filter appliedto the noise signal may depend on the operating event being monitored.For example, when monitoring valve 62, 64 events (e.g., openings andclosures), a high-pass filter (e.g., greater than 10 kilohertz (kHz)) ora band-pass filter (e.g., between 10 and 20 kilohertz (kHz)) may beapplied to the noise signal. When monitoring combustion events (e.g.,peak firing pressure), a low-pass filter (e.g., less than 2 kilohertz(kHz)) may be applied to the noise signal.

With reference to the process 88 shown in FIG. 7, the MIDI fingerprint100 having the ADSR envelope 82 information shown in FIG. 8 (e.g., withthe attack 83, decay 84, sustain 85, and release 86) may includeadditional information relating to the operating event beingfingerprinted or baselined. For example, during the process 88 (e.g.,baselining process), an operating event indicator 103 may also beplotted over the scaled/normalized engine noise plot 81. The operatingevent indicator 103, for example, may be a plot provided by a switch(e.g., limit switch) that modulates between high and low to indicate theoperating event during the baselining process (e.g., process 88). Forexample, the switch may be actuated each time the operating event occursduring the baselining process. However, in general, the switch may notbe included in the engine 10 during normal operation of the engine 10,as inclusion of both the switch and the knock sensor 23 may be redundantand expensive. Thus, the switch and the corresponding operating eventindicator 103 may be used during the baselining process (e.g., process88) to more accurately determine a location in the ADSR envelope 82 atwhich the operating event specifically occurs (e.g., within 2-4 degreescrankshaft 54 angle, depending on the operating event), such that theADSR envelope 82 can be stored to the ECU 25 and later utilized duringnormal operation of the engine 10 to determine a crankshaft 54 angle ortiming at which the operating event more specifically occurs within theADSR envelope 82.

In the illustrated embodiment, the operating event is a closure of theexhaust valve 64 shown in FIG. 2. As the exhaust valve 64 closes, theswitch is actuated, thereby causing the limit switch to move from low(e.g., low voltage) to high (e.g., high voltage). The switch transmits asignal of the operating event indicator 103 to the ECU 25, which mayplot the operating event indicator 103 on the scaled engine noise plot81. An intersecting point 105 between the operating event indicator 103and the ADSR envelope 82 may be stored along with the fingerprint 100corresponding to the operating event (e.g., the closure of the exhaustvalve 64). In the illustrated embodiment, the intersecting point 105 islocated at an approximate midpoint of the decay 84 vector (e.g., within5-10 percent of a length of the decay 84 vector from the midpoint). Ingeneral, closing of the exhaust valve 64 occurs at the midpoint ormid-region of the decay 84 vector (e.g., where the mid-region is an areadefined by 5-10 percent of a length of the decay 84 vector on eitherside of the midpoint of the decay 84 vector), and coordinates of themidpoint of the decay 84 vector can be calculated using a geometricmidpoint relationship, e.g., P_(i)=[(X₁+X₂)/2, (Y₁+Y₂)/2], where P_(i)is the midpoint (and, thus, the intersecting point 105), X₁ and X₂ arethe X coordinates along axis 76 at either end of the decay 84 vector,and Y₁ and Y₂ are the Y coordinates along axis 78 at either end of thedecay 84 vector. It should be noted that axis 78 in the illustratedembodiment includes time, but, in another embodiment, the axis 78 mayinclude crankshaft 54 angle (e.g., crank angle) information from thecrankshaft sensor 66, which is correlative of time.

After determining the intersection point 105 (which, in the illustratedembodiment relating to closure of the exhaust valve 64, is the midpointof the decay 84 vector of the ADSR envelope 82), the MIDI fingerprint100 (e.g., having the ADSR envelope 82 information and the intersectionpoint 105 information) may be stored for later analysis.

In some embodiments, it may be beneficial to check the MIDI fingerprint100 to ensure that the MIDI fingerprint 100 is accurate and can be usedto identify operating events during normal operation of the combustionengine 10. For example, FIG. 9 is a flow chart showing further detailsof an embodiment of process 102, which identifies and checks thefingerprint 100 depicted in FIG. 7. The process 102 may be implementedas computer instructions or executable code stored in the memory 74 andexecutable by the processor 72 of the ECU 25. In decision 104, the ECU25 determines whether or not the noise signal is modulating (i.e.,changing from one tone to another). If the signal is not modulating(decision 104), then the ECU 25 moves on to block 112 and attempts tofind a matching wavelet. A wavelet, effectively a piece or component ofa wave, is a wave-like oscillation with an amplitude that begins atzero, increases, decreases, or both, and then returns to zero. Waveletscan be modified by adjusting the frequency, amplitude, and duration,which makes them very useful in signal processing. For example, incontinuous wavelet transforms, a given signal may be reconstructed byintegrating over the various modified frequency components. Example“mother” wavelets include Meyer, Morlet, and Mexican hat wavelets.However, new wavelets may also be created if the mother wavelets do notfit.

If the sound is modulating (decision 104), the ECU 25 moves on todecision 108 and determines whether or not the noise signal fits achirplet. A chirp is a signal in which the frequency increases ordecreases with time. Just as a wavelet is a piece of a wave, a chirpletis a piece of a chirp. Much like wavelets, the characteristics of achirplet can be modified, and then multiple chirplets combined (i.e., achirplet transform), in order to approximate a signal. A chirplet maymodulate (i.e., change frequency) upward or downward. In decision 108,the ECU 25 may adjust the modulation of chirplets in order to fit thechirplets to the noise signal. If the ECU 25, after adjusting themodulation of chirplets, can adjust chriplets to fit the noise signal,then the ECU 25 logs whether there was a chirplet that fit the signal,and if so, the first frequency of the chirplet, the second frequency ofthe chirplet, and the rate of chirplet modulation in frequency/(crankangle) or frequency per second. The ECU 25 then moves to block 110, inwhich the ECU 25 phase shifts the noise signal in order to check thefingerprint 100. In block 110, the ECU 25 creates a generated noisesignal based upon the ASDR envelope 82 vectors or other components,extracted tonal information, and chirplet or wavelet fits. The ECU 25then shifts (block 110) the generated signal, e.g., 180 degrees out ofphase. If the characterization of the noise signal is correct, thephase-shifted generated noise signal should cancel out the noise signal.

If the noise signal does not fit a chirplet (decision 108), the ECU 25moves on to block 112 and attempts to fit a wavelet to the noise signal.In block 112, the ECU 25 selects one or more wavelets that may fit thenoise signal. The selected wavelet or wavelets may be a Meyer wavelet, aMorlet wavelet, a Mexican hat wavelet, or some other suitable wavelet.In decision 114, the ECU 25 determines whether or not the selectedwavelet or wavelets fits the noise signal. If the selected wavelet fits(decision 114), the ECU 25 logs that there was a wavelet fit, the motherwavelet type, the first scale range of the wavelet, and the second scalerange of the wavelet. If the wavelet fits (decision 114), the ECU 25moves on to block 110, in which the ECU 25 phase shifts the noise signalin order to check the fingerprint 100. If one of the selected waveletsdoes not fit the noise signal (decision 114), the ECU 25 may move on toblock 116 and create a wavelet. In decision 118, the ECU 25 determinesif the newly created wavelet fits the noise signal. If the createdwavelet fits (decision 118), the ECU 25 logs that there was a waveletfit, the first scale range of the wavelet, and the second scale range ofthe wavelet. If the created wavelet fits the noise signal (decision118), the ECU 25 moves on to block 110, in which the ECU phase shiftsthe noise signal in order to check the fingerprint 100. If the newwavelet does not fit (decision 118), the ECU 25 moves on to block 120 inwhich it characterizes the noise signal as broadband noise.

Returning now to block 110, if the ECU 25 finds a chirplet or waveletthat fits the noise signal, the ECU 25 may check the fit by attemptingnoise cancellation. Accordingly, in block 110, the ECU 25 creates agenerated noise signal based upon the ASDR envelope 82 vectors or othercomponents, extracted tonal information, and chirplet or wavelet fits.The ECU 25 then shifts (block 110) the generated signal by 180 degrees.The ECU 25 then determines (decision 122) whether the shifted signalcancels out the original noise signal within a desired residualtolerance. If the shifted signal cancels out (decision 122) the originalnoise signal within a desired residual tolerance, the ECU 25 determinesthat the fingerprint 100 is a “good” fingerprint 126 and moves on toblock 128, in which the ECU 25 logs the coefficients and associateddata, which may include the root mean squared (RMS) value of the signal,or the RMS error. The ECU 25 may log other data as well, including, butnot limited to crankshaft angles at the beginning or end of the signal,ASDR envelope 82 vectors or other ADSR components, fundamental spectraltones, harmonic spectral tones, order of spectral tones, order ofharmonic tones, whether a chirplet fit, the first chirplet frequency,the second chirplet frequency, the rate of chirplet modulation, whethera wavelet fit, the mother wavelet type, the first scale range of thewavelet, the second scale range of the wavelet, the maximum amplitudevalue and time, the minimum amplitude value and time, the RMS value ofthe signal, the RMS error of the signal against the generated signal,and whether or not the noise is classified as broadband noise. Further,as previously described, the ECU 25 may log the intersecting point 105on the ADSR envelope 82, as shown in FIG. 8. This logged data, and otherdata logged by the ECU 25, allows the ECU 25 to characterize andcategorize known noises (e.g., corresponding to certain operating eventsdescribed in the present disclosure) so these noises can be stored onthe memory component 74 of the ECU 25, perhaps transferred to some othermemory device, and then logged and sorted in a database for futureanalysis. If, on the other hand, the ECU 25 determines (decision 122)that the shifted signal did not cancel out the original noise signalwithin a residual tolerance, the ECU 25 moves on to block 124 in whichthe noise signal is characterized as broadband noise.

It should be noted that, depending on the embodiment, the process 102 inFIG. 9 may not be employed following the baselining method (e.g.,process 88). For example, in some embodiments, it may be determined thatthe fingerprint 100 is a “good fingerprint 126” without employingprocess 102. In either case, verified MIDI fingerprints 130 (e.g.,fingerprint 100 and/or good fingerprint 126) may be stored in a database132 for later access during an engine monitoring process 134, as shownin an embodiment of the process 134 in FIG. 10. For example, during theillustrated process 134, noise from the engine 10 is sensed (e.g.,detected or recorded) (block 136). As previously described, the noisemay be sensed via the knock sensor 23, or some other sensor configuredto detect noise or vibrations of the engine 10. The noise signal may bepreconditioned (e.g., scaled, normalized, and/or filtered) forprocessing, in accordance with the description of FIGS. 3-5. Thecrankshaft sensor 66 may also sense, detect, or record a position of thecrankshaft 54 (e.g., in crank angles). Accordingly, the noise signal(e.g., preconditioned noise signal) may be plotted, via the ECU 25,against the position of the crankshaft 54. As previously described, incertain embodiments, the noise signal may be plotted against timeinstead of position of the crankshaft 54.

The process 134 further includes accessing the MIDI fingerprints 130 inthe database 132 (block 138). For example, the ECU 25 may access thefingerprint 130 that relates to a particular operating event beingmonitored via the process 134. Depending on the embodiment, theoperating event (or condition) may be peak firing pressure, opening ofthe intake valve 62, closing of the intake valve 62, opening of theexhaust valve 64, closing of the exhaust valve 64, or some otheroperating event (or condition) of the engine 10.

After accessing the MIDI fingerprint 130 corresponding to the operatingevent (or condition) being monitored by the ECU 25 via process 134, theECU 25 may correlate the MIDI fingerprint 130 and the noise signal(e.g., preconditioned noise signal) to determine if the noise signalincludes a portion that matches the fingerprint 130. For example, aspreviously described, the MIDI fingerprint 130 may include the ADSRenvelope 82 relating to the operating event being monitored andgenerated during the baselining process (e.g., process 88). The ADSRenvelope 82 of the fingerprint 130 may be shifted or dragged along thetime or crankshaft 54 position axis of the noise signal (e.g.,preconditioned noise signal) to determine if the MIDI fingerprint 130matches any portion of the noise signal. For example, the ADSR envelope82 of the fingerprint 130 may be directly compared or matched withportions of the noise signal, or one or more operating ADSR envelopesmay be generated for portions of the noise signal (e.g., in accordancewith the descriptions of FIGS. 5 and 6) to compare with the ADSRenvelope 82 of the MIDI fingerprint 130. Further, in general, theoperating event may have occurred within a known range of time orcrankshaft 54 positions (e.g., in crank angles). Thus, the portion ofthe noise signal processed by the ECU 25 to determine whether a portionof the noise signal matches the MIDI fingerprint 130 may be reduced tothe known range of time or crankshaft 54 positions. It should be notedthat the match between the MIDI fingerprint 130 and the noise signal maynot be an exact match between the MIDI fingerprint 130 and the noisesignal (e.g., MIDI encoded noise signal). For example, the MIDIfingerprint 130 may substantially match a portion of the noise signaland may be rated by a percentage of accuracy of the match. A threshold(e.g., stored in the memory 74 of the ECU 25) may enable the ECU 25 todetermine if the percentage of accuracy of the match between the MIDIfingerprint 130 and the noise signal is substantial enough to considerthe MIDI fingerprint 130 and the noise signal a match. The threshold maybe at least equal to or greater than a 75% match, an 80% match, an 85%match, a 90% match, a 95% match, a 97% match, a 98% match, a 99% match,or a 100% match.

In decision 142, the ECU 25 determines if the MIDI fingerprint 130matches any portion of the noise signal (e.g., preconditioned noisesignal) from block 136. If the correlation in block 140 is a match indecision 142, the operating event being monitored is verified. Further,as shown in block 144, the particular location of the operating event(e.g., in time or in crank angles of the crankshaft 54) may bedetermined. For example, as previously described, the operating eventmay occur at the intersection point 105 (e.g., between the ADSR envelope82 and the operating event indicator 103) in FIG. 8, which, in someembodiments, corresponds to the midpoint on the decay 84 vector of theADSR envelope 82. Accordingly, the ECU 25 may overlay the ADSR envelope82 of the fingerprint 130 on the noise signal plotted against crankshaft54 position, and determine that the operating event occurred at thex-coordinate (e.g., time or crankshaft 54 position coordinate) of theintersection point 105 on the ADSR envelope 82.

If the MIDI fingerprint 130 is not matched with any portion of the noisesignal at decision 142, the process 134 may either return to block 136(e.g., sense engine noise) or return to block 138 (access fingerprint(s)in database). For example, in some embodiments, the process 134 may beutilized to monitor multiple operating events. Accordingly, the process134 may include accessing multiple fingerprints 130 for correlation withthe noise signal. The multiple fingerprints 130 may be accessed all inone step, or each fingerprint 130 may be accessed and then correlated tothe noise signal independently to determine and verify operating events.

In accordance with the present disclosure, it should be noted thatoperating event(s) and conditions may be any operating event orcondition of the engine 10. For example, the operating event may be anopening of the exhaust valve 64, a closing of the exhaust valve 64, anopening of the intake valve 62, a closing of the intake valve 62, peakfiring pressure, valve disconnect, valve lash or valve clearance issues(e.g., too much distance between certain valve train components such asrocker arms and valve tappet), or any other operating event of theengine 10. Further, it should be noted that the crank angle at which theoperating event occurs may be determined by the same or similar processsteps described above. For example, in some embodiments, the operatingevent may occur at a different point along the decay 84 vector, or alongone of the other vectors of the ADSR envelope 82. The operating eventindicator 103 shown in FIG. 8 may be provided to the ECU 25 by a limitswitch, or by some other mechanism configured to detect the operatingevent during the baselining process (e.g., process 88) that may not beincluded in the engine 10 during normal operation. Further, it should benoted that the fingerprints 100, 126, 130 associated with each operatingevent may vary for each operating event, and may vary for each model,make, or series of engines 10. Thus, the baselining process (e.g.,process 88) to determine fingerprints 100, 126, 130 for variousoperating events may be carried out for each particular engine 10, andeach engine 10 may include different MIDI fingerprints 100, 126, 130 forthe same operating event. Such fingerprinting may then be used in thefield to determine that the operating event has occurred. For example,noise from one or more knock sensors 23 may be compared againstfingerprints in the database 132 and matches used to determine thevarious operating events and/or engine conditions.

FIG. 11 is a flowchart illustrating an embodiment of a process 200suitable for applying MIDI techniques as described above. The process200 may be implemented as computer code or instructions stored in thememory 74 and executable via the processor 72. In the depictedembodiment, the process 200 may receive a vibration data (block 202),for example from one or more knock sensors 23. The vibration data may bereceived either during creation of the fingerprint 100 (e.g., at amanufacturer's laboratory, at a field site, or a combination thereof) orduring use of a fingerprint 100, 126 that has already been created, forexample, to use the fingerprint 100, 126 to determine that a certainevent has occurred (e.g. operating events and/or engine conditions).

The vibration data may then undergo MIDI conversion (block 204). Forexample, the vibration data may include a set of points in a timeline,each point representative of a sound frequency (e.g., in Hertz as partof sampled audio, which may be encoded as a WAV file, MP3 file, OggVorbis, file and so on). Sampled audio may be converted to MIDI (block204) through a variety of techniques, including converting chunks of theset of points in the timeline, each point in the timeline, or acombination thereof, into MIDI notes or note. For example, systems likeWIDI Recognition System Professional 4.03 available from WIDISOFT Co.,Live, available from Ableton AG, and so on, may be used to convertsampled vibrations into MIDI data 206.

Once converted, the MIDI data may be stored (block 208), for example, inthe memory 74 and/or in database system(s). Because of the sizereduction likely achieved by converting to MIDI data 206, storagerequirements may be minimized. The MIDI data 206 may alternatively oradditionally be transmitted (block 210). For example, the MIDI data 206may be transmitted to external systems for further analysis, to otherECUs 25 in a fleet of engines, to storage systems (e.g., cloud storagesystems), and so on. The MIDI data may also be processed further (block212), as described earlier, to derive scalings, fingerprints, waveletprocessing, and so on. Further, the MIDI data may be decompressed backto sampled vibrations, for example by converted the MIDI data to WAVdata, MP3 data, Ogg Vorbis data, and so on. For example, the noisesignal (e.g., vibration data 202) may be converted to MIDI data 206 andthen the MIDI data 206 correlated one or more MIDI fingerprints 100,126. Likewise, the one or more MIDI fingerprints 100, 126 may beconverted back to one or more vibration fingerprints (e.g., converted toWAV data, MP3 data, Ogg Vorbis data, and so on) and then the converteddata (e.g., vibration data 202) may be correlated to the noise signal.

Technical effects of the invention include characterizing a noise signaland deriving a MIDI signature or fingerprint from the noise signal,which may additionally include preconditioning the noise signal (e.g.,converting the signal to MIDI data), applying an ADSR envelope to thenoise signal, extracting tonal information (e.g., musical tones) fromthe noise signal and fitting the noise signal to a chirplet and/or awavelet. Further, technical effects of the invention may includedetermining a timing of particular operating events with respect tocrank angle based on the characterization of the noise signal andderivation of the signature(s) and/or fingerprints from the noisesignal.

This written description uses examples to disclose the invention,including the best mode, and also to enable any person skilled in theart to practice the invention, including making and using any devices orsystems and performing any incorporated methods. The patentable scope ofthe invention is defined by the claims, and may include other examplesthat occur to those skilled in the art. Such other examples are intendedto be within the scope of the claims if they have structural elementsthat do not differ from the literal language of the claims, or if theyinclude equivalent structural elements with insubstantial differencesfrom the literal language of the claims.

1. A method of monitoring an operating event of a combustion engine,comprising: receiving a noise signal sensed by a knock sensor disposedin or proximate to the combustion engine; correlating the noise signalwith a musical instrument digital interface (MIDI) fingerprint having atleast an ADSR envelope indicative of the operating event of thecombustion engine; and detecting if the operating event has occurredbased on the correlating of the noise signal with the fingerprint. 2.The method of claim 1, wherein the operating event comprises an openingof an intake valve of the internal combustion engine, a closing of theintake valve, an opening of an exhaust valve of the internal combustionengine, a closing of the exhaust valve, or a peak firing pressure. 3.The method of claim 1, comprising baselining the combustion engine toderive the MIDI fingerprint having at least the ADSR envelope indicativeof the operating event.
 4. The method of claim 3, wherein baselining thecombustion engine to derive the MIDI fingerprint having at least theADSR envelope comprises: deriving the ADSR envelope from a baselinenoise signal converted into a MIDI encoded baseline noise signalindicative of the operating event and plotting the ADSR envelope andoperating event indicator data against time to derive a location of theADSR envelope at which the operating event occurs.
 5. The method ofclaim 4, comprising deriving the location of the ADSR envelope at whichthe operating event occurs by determining an intersecting point betweenthe ADSR envelope and the operating event indicator data.
 6. The methodof claim 1, wherein correlating the noise signal with the MIDIfingerprint comprises converting the noise signal to a MIDI data andthen correlating the MIDI data to the MIDI fingerprint, converting theMIDI fingerprint to a vibration fingerprint and then correlating thenoise signal to the vibration fingerprint.
 7. The method of claim 4,wherein the location of the ADSR envelope at which the operating eventoccurs is approximately a midpoint of a decay vector of the ADSRenvelope.
 8. The method of claim 4, wherein the location of the ADSRenvelope at which the operating event occurs is within a mid-region of adecay vector of the ADSR envelope.
 9. The method of claim 1, whereincorrelating the noise signal with the MIDI fingerprint having at leastthe ADSR envelope indicative of the operating event comprisespreconditioning the noise signal and superimposing the ADSR envelopeonto at least a portion of a plot of the preconditioned noise signal.10. The method of claim 1, wherein correlating the noise signal with theMIDI fingerprint having at least the ADSR envelope indicative of theoperating event comprises plotting the noise signal, or a preconditionedversion of the noise signal, against a crank angle signal of acrankshaft of the combustion engine received from a crankshaft sensorand superimposing the ADSR envelope of the MIDI fingerprint onto atleast a portion of the plot.
 11. A system, comprising: an enginecontroller configured to monitor a first operating event of a combustionengine, wherein the engine controller comprises a processor configuredto: receive a noise signal sensed by a knock sensor disposed in orproximate to the combustion engine; correlate the noise signal with afirst musical instrument digital interface (MIDI) fingerprint having atleast a first ADSR envelope indicative of the first operating event; anddetect if the first operating event has occurred based on thecorrelating of the noise signal with the first MIDI fingerprint.
 12. Thesystem of claim 11, wherein the controller comprises a memory configuredto store one or more MIDI fingerprints, each MIDI fingerprint having arespective ADSR envelope indicative of a corresponding operating event,and wherein the processor is configured to access the memory tocorrelate the noise signal with the first MIDI fingerprint having atleast the first ADSR envelope indicative of the first operating event.13. The system of claim 11, comprising the knock sensor configured tosense the noise signal and a crankshaft sensor configured to sense acrank angle of a crankshaft of the combustion engine, and wherein theprocessor is configured to correlate the noise signal with the MIDIfingerprint by converting the noise signal to a MIDI data and thencorrelate the MIDI data to the MIDI fingerprint, wherein the processoris configured to convert the MIDI fingerprint to a vibration fingerprintand then correlate the noise signal to the vibration fingerprint, or acombination thereof.
 14. The system of claim 13, wherein the processoris configured to plot the noise signal, or a preconditioned version ofthe noise signal, against the crank angle, and superimpose the firstADSR envelope over the noise signal or preconditioned noise version ofthe noise signal.
 15. The system of claim 14, wherein the processor isconfigured to derive a location on the superimposed first ADSR envelopeat which the operating event occurs.
 16. The system of claim 15, whereinthe processor is configured to determine a midpoint of a decay vector ofthe superimposed first ADSR envelope, wherein the location on thesuperimposed first ADSR envelope at which the operating event occurs isthe midpoint.
 17. The system of claim 11, wherein the operating eventcomprises an opening of an intake valve of the combustion engine, aclosing of the intake valve, an opening of an exhaust valve of thecombustion engine, a closing of the exhaust valve, or a peak firingpressure.
 18. A non-transitory computer readable medium comprisingexecutable instructions that, when executed, cause a processor to:receive, from a knock sensor disposed in or proximate to a combustionengine, noise data indicative of noise emitted by the combustion engine;receive, from a crankshaft sensor disposed in or proximate to thecombustion engine, crank angle data indicative of a crank angle of acrankshaft of the combustion engine; plot the noise data against thecrank angle data; determine a portion of the noise data that correspondsto a musical instrument digital interface (MIDI) fingerprint having areference ADSR envelope indicative of an operating event of thecombustion engine; superimpose or plot the reference ADSR envelope overthe noise data; and determine a location in the noise data at which theoperating event occurred.
 19. The non-transitory computer readablemedium comprising executable instructions of claim 18 that, whenexecuted, further cause the processor to: determine a midpoint on adecay vector of the reference ADSR envelope, wherein the midpoint on thedecay vector of the reference ADSR envelope corresponds to the locationat which the operating event occurs.
 20. The non-transitory computerreadable medium comprising executable instructions of claim 18 that,when executed, further cause the processor to precondition the noisedata before plotting the noise data.